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Title:
飛行体の冷却システム
Document Type and Number:
Japanese Patent JP5208817
Kind Code:
B2
Abstract:

To achieve efficient thermal control by a simple configuration and an improved degree of freedom of an attachment arrangement including design.

An aerial 11 is arranged on an outer wall of a flight vehicle body 10, and a pressurized chamber 101 and an outside 102 of the pressurized chamber of the flight vehicle body 10 are communicated with a duct member 13. Air in the pressurized chamber 101 is flowed to the outside 102 of the pressurized chamber by using the pressure difference between the pressurized chamber 101 and the outside 102 of the pressurized chamber, the ambient temperature of the outside 102 of the pressurized chamber is cooled, a heat sink 12 thermally combined with a heat release face of the aerial 11 is blown by the air, and the aerial 11 is therefore thermally controlled.

COPYRIGHT: (C)2010,JPO&INPIT


Inventors:
Kenji Okubo
Application Number:
JP2009056928A
Publication Date:
June 12, 2013
Filing Date:
March 10, 2009
Export Citation:
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Assignee:
Toshiba Corporation
International Classes:
B64D47/00; B64D13/02
Domestic Patent References:
JP2007521183A
JP2005014627A
JP2003110330A
JP4081084U
JP2004028980A
JP2008258976A
JP8504704A
Foreign References:
US20050076661
US5327744
Attorney, Agent or Firm:
Kurata Masatoshi
Satoshi Kono
Makoto Nakamura
Yoshihiro Fukuhara
Takashi Mine
Toshio Shirane
Sadao Muramatsu
Nobuhisa Nogawa
Kocho Chojiro
Naoki Kono
Katsu Sunagawa
Tetsuya Kazama
Katsumura Hiro
Shoji Kawai
Tatsushi Sato
Takashi Okada
Mihoko Horiuchi
Takenori Masanori
Takuzo Ichihara
Yamashita Gen